SAE AMS 3281E-2010 Sealing Compound Polysulfide (T) Synthetic Rubber for Integral Fuel Tank and Fuel Cell Cavities Low Density for Intermittent Use to 360 F (182 C)《360F(182C)间歇性使用.pdf
《SAE AMS 3281E-2010 Sealing Compound Polysulfide (T) Synthetic Rubber for Integral Fuel Tank and Fuel Cell Cavities Low Density for Intermittent Use to 360 F (182 C)《360F(182C)间歇性使用.pdf》由会员分享,可在线阅读,更多相关《SAE AMS 3281E-2010 Sealing Compound Polysulfide (T) Synthetic Rubber for Integral Fuel Tank and Fuel Cell Cavities Low Density for Intermittent Use to 360 F (182 C)《360F(182C)间歇性使用.pdf(16页珍藏版)》请在麦多课文档分享上搜索。
1、_ SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising there
2、from, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 20 SAE International All rights reserved. No part of this publication may
3、 be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: 724-776-4970 (outside USA) F
4、ax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AMS3281E AEROSPACE MATERIAL SPECIFICATION AMS3281 REV. E Issued 1994-11 Revised 2010-12Superseding
5、 AMS3281D Sealing Compound, Polysulfide (T) Synthetic Rubber for Integral Fuel Tank and Fuel Cell Cavities Low Density for Intermittent Use to 360 F (182 C) RATIONALE Resistance to thermal rupture was removed from initial acceptance testing and specific gravity is added to initial acceptance testing
6、. Several formatting changes were also made to bring the specification more in-line with current standards. 1. SCOPE 1.1 Form This specification covers three types and three classes of fuel-resistant polysulfide (T) sealing compound with low specific gravity, supplied as a two-component system which
7、 cures at room temperature. 1.2 Application This sealing compound has been used typically in sealing aircraft integral fuel tanks, fuel tank fillets and faying surfaces, pressure barriers and moldline surfaces, but usage is not limited to such applications. The sealing compound is resistant to jet f
8、uels and is capable of withstanding long-term exposure from -65 to +250 F (-54 to +121 C) and short-term exposure (6 hours) to 360 F (182 C). 1.3 Classification Type 1 - Sealing compound with a specific gravity of 1.20 to 1.35. Type 2 - Sealing compound with a specific gravity of 1.06 to 1.19. Type
9、3 - Sealing Compound with a specific gravity of 1.05 or less. 1.3.1 Sealing compounds covered by this specification are classified by method of application and application times as follows: Class A Suitable for application by brushing, injecting, or spraying. Available with the following application
10、 times in hours: A-1/2 A-2 Class B Suitable for application by extrusion gun or spatula. Available with the following application times in hours: B-1/2 B-2 10Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from I
11、HS-,-,-SAE AMS3281E Page 2 of 16Class C Suitable for faying surface or shim sealing, brush coating, or wet installation. Available with the following application times in hours: Notation: ( ) Assembly time in hours. C-2(2) C-8(24) C-12(48) C-48(168) C-96(336) 1.4 Safety - Hazardous Materials Shall b
12、e in accordance with AS5502 (1.1). 2. APPLICABLE DOCUMENTS Shall be in accordance with AS5502 (2.). 2.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), or www.sae.org.AMS247
13、1 Anodic Treatment of Aluminum Alloys, Sulfuric Acid Process, Undyed Coating AMS2629 Fluid, Jet Reference AMS3020 Oil, Reference, for “L” Stock Rubber Testing AMS3021 Fluid, Reference, for Testing Di-ester (Polyol) Resistant Material AMS3100 Adhesion Promoter, for Polysulfide Sealing Compounds AMS32
14、76 Sealing Compound, Integral Fuel Tanks and General Purpose, Intermittent Use to 360 F (182 C) AMS4045 Aluminum Alloy Sheet and Plate, 5.6Zn - 2.5Mg - 1.6 Cu - 0.23 Cr, 7075: (-T6 Sheet, -T651 Plate), Solution and Precipitation Heat Treated AMS4911 Titanium Alloy, Sheet, Strip, and Plate, 6Al - 4V,
15、 Annealed AMS5516 Steel, Corrosion-Resistant, Sheet, Strip, and Plate, 18Cr - 9.0Ni (SAE 30302), Solution Heat Treated AMS-C-27725 Coating, Corrosion Preventive, for Aircraft Integral Fuel Tanks for Use to 250 F (121 C) AS5127 Methods for Testing Aerospace Sealants AS5127/1 Aerospace Standard Test M
16、ethods for Aerospace Sealants, Two-Component Synthetic Rubber Compounds AS5502 Standard Requirements for Aerospace Sealants Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS3281E Page 3 of 162.
17、2 U.S. Government Publications Available from the Document Automation and Production Service (DAPS), Building 4/D, 700 Robbins Avenue, Philadelphia, PA 19111-5094, Tel: 215-697-6257, http:/assist.daps.dla.mil/quicksearch/.MIL-PRF-23377 Primer Coatings: Epoxy Polyamide, Chemical and Solvent Resistant
18、 MIL-DTL-81706 Chemical Conversion Materials for Coating Aluminum and Aluminum Alloys MIL-PRF-85285 Coating, Polyurethane, High Solids MIL-PRF-85582 Primer Coatings, Epoxy, Waterborne 2.3 PRI Publications Available from PRI, 161 Thorn Hill Road, Warrendale, PA 15086-7527, Tel: 724-772-1616, www.pri-
19、network.org.PD 2000 Procedures for an Industry Qualified Product Management Process 3. TECHNICAL REQUIREMENTS 3.1 Materials The basic ingredient shall be synthetic rubber, made from liquid polysulfide and derivations thereof. The sealing compound shall cure by the addition of a separate curing agent
20、 to the base compound and shall not depend on solvent evaporation for curing. The curing agent shall possess sufficient color contrast to the base compound to permit easy identification of an unmixed or incompletely mixed sealing compound. Neither the base compound nor the cured sealing compound sha
21、ll be red or pink in color. No glass fillers shall be used. 3.1.1 Qualification All products sold to this specification shall be listed, or approved for listing, on the PRI qualified products list. The qualified products list shall be in accordance with PD 2000. 3.2 Date of Packaging Shall be in acc
22、ordance with AS5502 (3.1). 3.3 Toxicological Formulations Shall be in accordance with AS5502 (3.2). 3.4 Quality Shall be in accordance with AS5502 (3.3). 3.5 Shelf Life Shelf life shall be a minimum of 9 months from the date of packaging. Material may be retested for shelf life extension. 3.5.1 Prem
23、ixed and Frozen Material Premixed and frozen material shall have a minimum storage life of 42 days at -80 F (-62 C) or lower, or 30 days at -40 F (-40 C) or lower, or 10 days at -10 to -40 F (-23 to -40 C) from date of mix/freeze. The date of mix/freeze shall be within the shelf life of the unmixed
24、material. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE AMS3281E Page 4 of 163.6 Properties The base compound and the curing agent, when mixed in accordance with manufacturers instructions and
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